EP0153473A2 - Cast aluminium pistons for internal-combustion engines with a mechanically densified surface of the pin bores - Google Patents

Cast aluminium pistons for internal-combustion engines with a mechanically densified surface of the pin bores Download PDF

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Publication number
EP0153473A2
EP0153473A2 EP84115436A EP84115436A EP0153473A2 EP 0153473 A2 EP0153473 A2 EP 0153473A2 EP 84115436 A EP84115436 A EP 84115436A EP 84115436 A EP84115436 A EP 84115436A EP 0153473 A2 EP0153473 A2 EP 0153473A2
Authority
EP
European Patent Office
Prior art keywords
hub
rolling
combustion engines
aluminum
hub bore
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP84115436A
Other languages
German (de)
French (fr)
Other versions
EP0153473A3 (en
EP0153473B1 (en
Inventor
Hans-Jürgen Köhnert
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mahle GmbH
Original Assignee
Mahle GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mahle GmbH filed Critical Mahle GmbH
Publication of EP0153473A2 publication Critical patent/EP0153473A2/en
Publication of EP0153473A3 publication Critical patent/EP0153473A3/en
Application granted granted Critical
Publication of EP0153473B1 publication Critical patent/EP0153473B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/10—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass pistons
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00—Pistons 
    • F02F3/0015—Multi-part pistons
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16J—PISTONS; CYLINDERS; SEALINGS
    • F16J1/00—Pistons; Trunk pistons; Plungers
    • F16J1/10—Connection to driving members
    • F16J1/14—Connection to driving members with connecting-rods, i.e. pivotal connections
    • F16J1/16—Connection to driving members with connecting-rods, i.e. pivotal connections with gudgeon-pin; Gudgeon-pins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00—Metals
    • F05C2201/02—Light metals
    • F05C2201/021—Aluminium
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49249—Piston making
    • Y10T29/49256—Piston making with assembly or composite article making

Definitions

  • the invention relates to a cast aluminum piston for internal combustion engines according to the preamble of claim 1.
  • the object of the invention is to design the hub bores even more securely against hub cracks.
  • This training can be achieved in particular by a method according to claim 2.
  • Claim 3 shows the best possible condition of the hub bore for the machining according to the invention.
  • the loss of effectiveness of the previous measures under extremely high loads is based on the following circumstance. If the material in the hubs of the piston reaches temperatures between 200 ° and 250 ° C, the cold-formed structure begins to grow quite rapidly due to recrystallization or recovery processes. It is a structural change. This increases the volume of the compressed area. As a result, additional compressive residual stresses caused by the growth develop in addition to the residual compressive stresses introduced. These can reach very high values. This finally leads to the fact that the total residual compressive stresses occurring in the compressed zone add up so high that shear stress cracks occur.
  • the surface zone in the hub bores is therefore not strain hardened. Rather, the surface is rolled at an elevated temperature at which the microstructure can be changed without introducing residual stresses.
  • the fiber direction in the circumferential direction ie. H. align each tangent to this. This is practically an elastic deformation in the circumferential direction.
  • this circumferentially aligned fiber course brings about the desired increase in strength, which does not lose its effect even at material temperatures between 200 ° and 250 ° C. This is essentially due to the fact that when compression occurs under heat with simultaneous fiber alignment, no residual compressive stresses are introduced into the material.
  • the hub bores are pre-turned to a diameter which is approximately 0.4 mm smaller than the diameter of the finished hub bore.
  • the pre-turned hub bore is rolled by an amount at a temperature of 450 ° C expanded by 0.2 mm in diameter.
  • the deformation zone within which the structure of the aluminum alloy is aligned in the circumferential direction of the hub bore that is to say in which a fiber course is produced which is oriented in the circumferential direction of the hub bore, measures approximately 0.35 mm in radial depth. Then the hub bore is turned to the finished dimension. Post-processing of the hub bore after rolling is necessary because the widening is different over the length of the hub bore, ie the hub bore widens more at the ends than in the middle.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

Bei einem gegossenen Aluminiumkolben für Verbrennungsmotoren mit mechanisch verdichteten Nabenbohrungs-Innenflächen weist das unterhalb dieser Innenflächen liegende Gefüge des Aluminiummaterials auf einer radialen Tiefe von mindestens 0,1 mm, vorzugsweise 0,2 mm, einen in Umfangsrichtung der Nabenbohrung ausgerichteten Faserverlauf auf. Erzielt wird dieser F Aserverlauf durch Walzen bei einer Temperatur von mindestens 350° C bis 400° C bei gleichzeitiger Aufweitung der Bohrung um etwa 0,2 bis 0,5 mm.In the case of a cast aluminum piston for internal combustion engines with mechanically compressed inner surface of the bore, the structure of the aluminum material lying below these inner surfaces has a radial fiber orientation of at least 0.1 mm, preferably 0.2 mm, in the circumferential direction of the inner bore. This fiber course is achieved by rolling at a temperature of at least 350 ° C to 400 ° C while simultaneously expanding the bore by about 0.2 to 0.5 mm.

Description

Die Erfindung betrifft einen gegossenen Aluminium-Kolben für Verbrennungsmotoren nach dem Oberbegriff des Anspruchs 1.The invention relates to a cast aluminum piston for internal combustion engines according to the preamble of claim 1.

Es ist bekannt, z. B. aus US 4,124,010, das gegossene Aluminiummaterial in den Nabenbohrungen längs deren Umfangfläche mechanisch oberflächlich zu verdichten. Dieses Verdichten erfolgt durch aufweitendes Walzen bei Raumtemperatur des Kolbens. Durch ein solches Verdichten läßt sich die Festigkeit des Aluminiummaterials im Bereich der Nabenbohrungsoberfläche erhöhen, d.h. die Nabenbohrungen können dadurch in ihrer Sicherheit gegenüber an der Nabenbohrung ausgehenden Nabenrissen erhöht werden. Bei relativ hohen Kolbenbelastungen haben sich die bisherigen Maßnahmen zur Erhöhung der Nabenrißfestigkeit jedoch als nicht ausreichend erwiesen.It is known e.g. B. from US 4,124,010 to mechanically compress the cast aluminum material in the hub bores along the circumferential surface thereof. This compression takes place by expanding rolling at room temperature of the piston. Such compacting increases the strength of the aluminum material in the area of the hub bore surface, i.e. the hub bores can thereby be increased in their security in relation to hub cracks starting at the hub bore. With relatively high piston loads, however, the previous measures for increasing the hub crack resistance have not proven to be sufficient.

Hiervon ausgehend liegt der Erfindung die Aufgabe zugrunde, die Nabenbohrungen noch sicherer gegen Nabenrisse auszulegen.Proceeding from this, the object of the invention is to design the hub bores even more securely against hub cracks.

Gelöst wird-diese Aufgabe durch eine Ausbildung des Aluminiummaterials im Bereich der Nabenbohrungsumfangsfläche nach den Merkmalen des kennzeichnenden Teils des Anspruchs 1.This object is achieved by designing the aluminum material in the area of the hub bore circumferential surface in accordance with the features of the characterizing part of claim 1.

Erreicht kann diese Ausbildung insbesondere durch ein Verfahren nach dem Anspruch 2 werden.This training can be achieved in particular by a method according to claim 2.

Den bestmöglichen Zustand der Nabenbohrung für die erfindungsgemäße Bearbeitung gibt der Anspruch 3 wieder.Claim 3 shows the best possible condition of the hub bore for the machining according to the invention.

Die Erklärung für den erfindungsgemäß erzielbaren Erfolg ist in folgendem zu sehen.The explanation for the success achievable according to the invention can be seen in the following.

Das eingangs zum Stand der Technik genannte Kaltverdichten der Oberfläche der Nabenbohrungen durch Walzen bewirkt in einer äußerst geringen Oberflächentiefe Druckeigenspannungen. Wenn diese Druckeigenspannungen nicht übermäßig hoch sind, können sie sich durchaus positiv auf die Nabenfestigkeit auswirken. Daher wird in der Praxis bisher auch sehr häufig von dieser Methode Gebrauch gemacht. Bei extrem hohen Belastungen hat sich jedoch herausgestellt, daß die gewünschte und erhoffte Festigkeitssteigerung nicht eintritt. Eine Erklärung hierfür gab es bisher allerdings nicht. Deshalb gilt in der Praxis das sog. Kalt-Walzverdichten immer noch als eine der gängigen Methoden zur Steigerung der Nabenfestigkeit.The cold compression of the surface of the hub bores by rolling, which was mentioned at the beginning of the prior art, causes residual compressive stresses in an extremely small surface depth. If these residual compressive stresses are not excessively high, they can have a positive effect on the hub strength. For this reason, this method has been used very frequently in practice. With extremely high loads, however, it has been found that the desired and hoped-for increase in strength does not occur. So far, however, there has been no explanation for this. That is why in practice the so-called cold roll compaction is still one of the common methods for increasing the hub strength.

Mit dem Wissen nach der vorliegenden Erfindung beruht der Wirkverlust der bisherigen Maßnahmen bei extrem hoher Belastung auf folgendem Umstand. Erreicht das Material in den Naben des Kolbens Temperaturen zwischen 200° und 250°C, so beginnt die kaltverformte Gefügestruktur durch Rekristallisation bzw. Erholungsprozesse recht stark zu wachsen. Es handelt sich dabei um eine Gefügeumwandlung. Damit nimmt das Volumen des verdichteten Bereiches zu. Als Folge bilden sich zu den eingebrachten Druckeigenspannungen noch zusätzliche durch das Wachsen bedingte Druckeigenspannungen aus. Diese können sehr hohe Werte erreichen. Dies führt dann schließlich dazu, daß die insgesamt in der verdichteten Zone auftretenden Druckeigenspannungen sich so hoch aufsummieren, daß Schubspannungsrisse entstehen.With the knowledge of the present invention, the loss of effectiveness of the previous measures under extremely high loads is based on the following circumstance. If the material in the hubs of the piston reaches temperatures between 200 ° and 250 ° C, the cold-formed structure begins to grow quite rapidly due to recrystallization or recovery processes. It is a structural change. This increases the volume of the compressed area. As a result, additional compressive residual stresses caused by the growth develop in addition to the residual compressive stresses introduced. These can reach very high values. This finally leads to the fact that the total residual compressive stresses occurring in the compressed zone add up so high that shear stress cracks occur.

Dieser Mechanismus ist vor allem bei AlSi-Legierungen besonders stark ausgeprägt. Ist das Material infolge zu hoher Druckeigenspannungen, wie sie im Motorbetrieb bei hohen Temperaturen auftreten, gefügemäßig einmal bereits vorgeschädigt, dann treten die eigentlich durch ein Kaltverdichten zu vermeidenden Nabenrisse im Prinzip noch eher auf als in unverdichtetem Material.This mechanism is particularly pronounced with AlSi alloys. If the material has already been damaged as a result of excessive residual compressive stresses, such as occur in engine operation at high temperatures, then the hub cracks that are actually to be avoided by cold compression occur in principle even earlier than in non-compressed material.

Bei der erfindungsgemäßen Lösung wird daher eine Kaltverfestigung der Oberflächenzone in den Nabenbohrungen nicht vorgenommen. Es erfolgt vielmehr ein Walzen der Oberfläche unter einer erhöhten Temperatur, bei der die Gefügestruktur ohne das Einbringen von Eigenspannungen verändert werden kann. Auf diese Weise läßt sich in ausreichender Tiefe des Materials der Faserverlauf in Umfangsrichtung, d. h. jeweils tangetial zu dieser, ausrichten. Dies ist praktisch eine elastische Verformung in Umfangsrichtung. Dieser umfangsmäßig ausgerichtete Faserverlauf bewirkt nach der Erfindung die angestrebte Festigkeitserhöhung, die auch bei Materialtemperaturen zwischen 200° und 250°C ihre Wirkung nicht verliert. Dies beruht im wesentlichen darauf, daß bei der unter Wärme erfolgten Verdichtung bei gleichzeitiger Faserausrichtung keine Druckeigenspannungen in das Material eingebracht werden.In the solution according to the invention, the surface zone in the hub bores is therefore not strain hardened. Rather, the surface is rolled at an elevated temperature at which the microstructure can be changed without introducing residual stresses. In this way, the fiber direction in the circumferential direction, ie. H. align each tangent to this. This is practically an elastic deformation in the circumferential direction. According to the invention, this circumferentially aligned fiber course brings about the desired increase in strength, which does not lose its effect even at material temperatures between 200 ° and 250 ° C. This is essentially due to the fact that when compression occurs under heat with simultaneous fiber alignment, no residual compressive stresses are introduced into the material.

Ein Ausführungsbeispiel der Erfindung wird nachfolgend beschrieben.An embodiment of the invention is described below.

Bei einem gegossenen Kolben aus einer AlSi-Legierung werden die Nabenbohrungen vorgedreht auf einen Durchmesser der um etwa 0,4 mm kleiner als der Durchmesser der fertigbearbeiteten Nabenbohrung ist. Die vorgedrehte Nabenbohrung wird bei einer Temperatur von 450°C durch Walzen um einen Betrag von 0,2 mm im Durchmesser aufgeweitet. Die Verformungszone, innerhalb der das Gefüge der Aluminium-Legierung in Umfangsrichtung der Nabenbohrung ausgerichtet wird, d. h. in dem ein in Umfangsrichtung der Nabenbohrung ausgeriteter Faserverlauf erzeugt wird, mißt in radialer Tiefe etwa 0,35 mm. Danach wird die Nabenbohrung auf Fertigmaß gedreht. Die Nachbearbeitung der Nabenbohrung nach dem Walzen ist erforderlich, da die Aufweitung über die Länge der Nabenbohrung unterschiedlich ist, d. h. die Nabenbohrung weitet sich an den Enden stärker als in der Mitte auf.In the case of a cast piston made of an AlSi alloy, the hub bores are pre-turned to a diameter which is approximately 0.4 mm smaller than the diameter of the finished hub bore. The pre-turned hub bore is rolled by an amount at a temperature of 450 ° C expanded by 0.2 mm in diameter. The deformation zone within which the structure of the aluminum alloy is aligned in the circumferential direction of the hub bore, that is to say in which a fiber course is produced which is oriented in the circumferential direction of the hub bore, measures approximately 0.35 mm in radial depth. Then the hub bore is turned to the finished dimension. Post-processing of the hub bore after rolling is necessary because the widening is different over the length of the hub bore, ie the hub bore widens more at the ends than in the middle.

Claims (3)

1.) Aluminiumkolben, insbesondere aus einer gegossenen AlSi-Legierung, für Verbrennungsmotoren, bei dem das Aluminiummaterial an den inneren Umfangsflächen der Nabenbohrungen mechanisch durch Oberflächenbehandlung verdichtet ist,
dadurch gekennzeichnet ,
daß das Gefüge des Aluminiummaterials frei von Druckeigenspannungen ist und auf einer radialen Tiefe von mindestens 0,1 mm, vorzugsweise 0,2 mm-, einen in Umfangsrichtung der Nabenbohrung ausgerichteten Faserverlauf aufweist.1.) aluminum pistons, in particular made of a cast AlSi alloy, for internal combustion engines in which the aluminum material on the inner peripheral surfaces of the hub bores is mechanically compressed by surface treatment,
characterized ,
that the structure of the aluminum material is free from residual compressive stresses and has a fiber orientation oriented in the circumferential direction of the hub bore at a radial depth of at least 0.1 mm, preferably 0.2 mm. 2.) Verfahren zur Herstellung eines Aluminiumkolbens nach Anspruch 1,
dadurch gekennzeichnet ,
daß die Gefügeverformung durch ein Walzen bei einer Temperatur von mindestens 350°C. vorzugsweise über 400°C, erfolgt, wobei die Nabenbohrung gleichzeitig im Durchmesser um einen Betrag von 0,2 - 0,5 mm aufgeweitet wird.2.) Method for producing an aluminum piston according to claim 1,
characterized ,
that the structural deformation by rolling at a temperature of at least 350 ° C. preferably above 400 ° C, the hub bore being simultaneously widened in diameter by an amount of 0.2-0.5 mm. 3.) Verfahren nach Anspruch 2,
dadurch gekennzeichnet ,
daß die Gefügeverformung durch Walzen an der bereits vorgedrehten jedoch noch mit einer Bearbeitungszugabe versehenen Nabenbohrung erfolgt, wobei das radiale Maß der Bearbeitungszugabe derart vorgegeben ist, daß nach dem Walzen noch über die gesamte Länge und den gesamten Umfang der Nabenbohrung eine Materialabtragung in die verformte Zone des Aluminiummaterials hinein erfolgen kann.3.) Method according to claim 2,
characterized ,
that the structural deformation takes place by rolling on the already pre-turned but still provided with a machining allowance, the radial dimension of the machining allowance being predetermined such that after rolling, material removal into the deformed zone of the hub bore over the entire length and the entire circumference Aluminum material can be done.
EP84115436A 1984-02-11 1984-12-14 Cast aluminium pistons for internal-combustion engines with a mechanically densified surface of the pin bores Expired - Lifetime EP0153473B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19843404903 DE3404903A1 (en) 1984-02-11 1984-02-11 MOLDED ALUMINUM PISTON FOR COMBUSTION ENGINES WITH SURFACE MECHANICALLY COMPRESSED HUB HOLES
DE3404903 1984-02-11

Publications (3)

Publication Number Publication Date
EP0153473A2 true EP0153473A2 (en) 1985-09-04
EP0153473A3 EP0153473A3 (en) 1987-08-12
EP0153473B1 EP0153473B1 (en) 1991-08-28

Family

ID=6227449

Family Applications (1)

Application Number Title Priority Date Filing Date
EP84115436A Expired - Lifetime EP0153473B1 (en) 1984-02-11 1984-12-14 Cast aluminium pistons for internal-combustion engines with a mechanically densified surface of the pin bores

Country Status (5)

Country Link
US (1) US4633764A (en)
EP (1) EP0153473B1 (en)
JP (1) JPS60209650A (en)
BR (1) BR8500563A (en)
DE (2) DE3404903A1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0809050A1 (en) * 1996-05-20 1997-11-26 Yamaha Hatsudoki Kabushiki Kaisha Piston for an internal combustion engine and method of making a piston
US5972071A (en) * 1997-07-17 1999-10-26 Yamaha Hatsudoki Kabushiki Kaisha Aluminum alloy for piston and method for producing piston
US6032570A (en) * 1998-04-10 2000-03-07 Yamaha Hatsudoki Kabushiki Kaisha Composite piston for machine
US6205836B1 (en) 1998-07-09 2001-03-27 Yamaha Hatsudoki Kabushiki Kaisha Method for manufacturing piston by forging and forging die
US6240827B1 (en) 1997-04-10 2001-06-05 Yamaha Hatsudoki Kabushiki Kaisha Composite piston for reciprocating machine
US6363608B1 (en) 1997-04-10 2002-04-02 Yamaha Hatsudoki Kabushiki Kaisha Method of manufacturing piston
DE10141189A1 (en) * 2001-08-22 2003-03-20 Ks Kolbenschmidt Gmbh Internal combustion engine piston shaft has shaft part remodeled by friction welding to form cast or conversion matrices specifically as piston boss.

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19837596C1 (en) * 1998-08-19 2000-01-05 Ks Kolbenschmidt Gmbh Light-metal piston for internal combustion engine
DE19956425A1 (en) * 1999-11-24 2001-05-31 Mahle Gmbh Piston for IC engines uses Laser beams to roughen bearings for gudgeon pin or crankshaft at points of max.load
WO2003010429A1 (en) * 2001-07-23 2003-02-06 Showa Denko K.K. Forged piston for internal combustion engine and manfacturing method thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1822877A (en) * 1928-12-22 1931-09-15 Aluminum Co Of America Method of treating aluminum base alloys which are subject to growth
US3014771A (en) * 1958-05-21 1961-12-26 Alco Products Inc Pistons
US3324772A (en) * 1964-05-29 1967-06-13 Karl Schmidt G M B H Fa Piston
US3473209A (en) * 1965-09-13 1969-10-21 Int Harvester Co Method to relieve pin bore of pistons
JPS50103458A (en) * 1974-01-18 1975-08-15
US4124010A (en) * 1976-12-20 1978-11-07 Dana Corporation Piston pin bore and method of finishing

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0809050A1 (en) * 1996-05-20 1997-11-26 Yamaha Hatsudoki Kabushiki Kaisha Piston for an internal combustion engine and method of making a piston
US5992015A (en) * 1996-05-20 1999-11-30 Yamaha Hatsudoki Kabushiki Kaisha Process for forming composite piston
US6209446B1 (en) 1996-05-20 2001-04-03 Yamaha Hatsudoki Kabushiki Kaisha Piston for internal combustion engine and process of making same
US6240827B1 (en) 1997-04-10 2001-06-05 Yamaha Hatsudoki Kabushiki Kaisha Composite piston for reciprocating machine
US6363608B1 (en) 1997-04-10 2002-04-02 Yamaha Hatsudoki Kabushiki Kaisha Method of manufacturing piston
US5972071A (en) * 1997-07-17 1999-10-26 Yamaha Hatsudoki Kabushiki Kaisha Aluminum alloy for piston and method for producing piston
US6032570A (en) * 1998-04-10 2000-03-07 Yamaha Hatsudoki Kabushiki Kaisha Composite piston for machine
US6205836B1 (en) 1998-07-09 2001-03-27 Yamaha Hatsudoki Kabushiki Kaisha Method for manufacturing piston by forging and forging die
DE10141189A1 (en) * 2001-08-22 2003-03-20 Ks Kolbenschmidt Gmbh Internal combustion engine piston shaft has shaft part remodeled by friction welding to form cast or conversion matrices specifically as piston boss.

Also Published As

Publication number Publication date
JPS60209650A (en) 1985-10-22
US4633764A (en) 1987-01-06
EP0153473A3 (en) 1987-08-12
EP0153473B1 (en) 1991-08-28
DE3484990D1 (en) 1991-10-02
DE3404903A1 (en) 1985-08-14
BR8500563A (en) 1985-09-24

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